DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE:
CHAPTERPAGE 335
MAINTENANCE MANUAL STEMME S12
3.6 FLIGHT CONTROL INSTRUMENTS, PITOT STATIC SYSTEM
Instruments: See Equipment List.
CAUTION
For modications sections 3.8 and 9 must be respected.
Pitot pressure, static pressure and total energy compensation are measured by means of a
multi-purpose probe in the nose-cone. Its orices are plumbed to the instrument panel through
the nose-cone sliding tube.
NOTICE
Some instruments, e. g. Bohli-diaphragm-type rate-of-climb indicator, need additional static ports
for proper operation at the widest area of the forward fuselage. These additional static ports are
installed only, if they were required for instrumentation at time of delivery.
All hose lines of the pitot-static system are equipped with a water separator/lter in the front
cockpit area below the instrument panel.
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